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Aeroelastic Wing Shaping Using Distributed PropulsionAn aircraft has wings configured to twist during flight. Inboard and outboard propulsion devices, such as turbofans or other propulsors, are connected to each wing, and are spaced along the wing span. A flight controller independently controls thrust of the inboard and outboard propulsion devices to significantly change flight dynamics, including changing thrust of outboard propulsion devices to twist the wing, and to differentially apply thrust on each wing to change yaw and other aspects of the aircraft during various stages of a flight mission. One or more generators can be positioned upon the wing to provide power for propulsion devices on the same wing, and on an opposite wing.
Document ID
20170009508
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Nguyen, Nhan T.
Reynolds, Kevin Wayne
Ting, Eric B.
Date Acquired
October 4, 2017
Publication Date
September 5, 2017
Subject Category
Aircraft Propulsion And Power
Aircraft Design, Testing And Performance
Report/Patent Number
Patent Number: US-Patent-9,751,614
Patent Application Number: US-Patent-Appl-SN-14/986,011
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-9,751,614
Patent Application
US-Patent-Appl-SN-14/986,011
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